EP1803645B1 - Module pour un aéronef - Google Patents
Module pour un aéronef Download PDFInfo
- Publication number
- EP1803645B1 EP1803645B1 EP05028664.0A EP05028664A EP1803645B1 EP 1803645 B1 EP1803645 B1 EP 1803645B1 EP 05028664 A EP05028664 A EP 05028664A EP 1803645 B1 EP1803645 B1 EP 1803645B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- aircraft
- frame device
- module
- frame
- floor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Not-in-force
Links
- 238000000034 method Methods 0.000 claims description 17
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 12
- 229910052760 oxygen Inorganic materials 0.000 claims description 12
- 239000001301 oxygen Substances 0.000 claims description 12
- 238000009434 installation Methods 0.000 description 8
- 238000010276 construction Methods 0.000 description 7
- 230000005484 gravity Effects 0.000 description 6
- 230000001133 acceleration Effects 0.000 description 4
- 230000005611 electricity Effects 0.000 description 3
- 239000011295 pitch Substances 0.000 description 3
- 238000001816 cooling Methods 0.000 description 2
- 230000003028 elevating effect Effects 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229920000271 Kevlar® Polymers 0.000 description 1
- 230000004308 accommodation Effects 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 238000003491 array Methods 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000004438 eyesight Effects 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 230000004313 glare Effects 0.000 description 1
- 239000004761 kevlar Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 1
- 229920002492 poly(sulfone) Polymers 0.000 description 1
- 238000010926 purge Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000000153 supplemental effect Effects 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/003—Stowage devices for passengers' personal luggage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/18—Floors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/0015—Arrangements for entertainment or communications, e.g. radio, television
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/0015—Arrangements for entertainment or communications, e.g. radio, television
- B64D11/00154—Loudspeakers mounted in the seat back
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0601—Arrangement of seats for non-standard seating layouts, e.g. seats staggered horizontally or vertically, arranged in an angled or fishbone layout, or facing in other directions than the direction of flight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0602—Seat modules, i.e. seat systems including furniture separate from the seat itself
- B64D11/0604—Seat modules, i.e. seat systems including furniture separate from the seat itself including a bed, e.g. cocoon type passenger seat modules
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0611—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with means for holding the passenger in a standing position
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0626—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with individual temperature or ventilation control
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0627—Seats combined with storage means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0627—Seats combined with storage means
- B64D11/0629—Seats combined with storage means the storage means being specially adapted for emergency equipment
- B64D11/0631—Seats combined with storage means the storage means being specially adapted for emergency equipment for life vests
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0639—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with features for adjustment or converting of seats
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0639—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with features for adjustment or converting of seats
- B64D11/06395—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with features for adjustment or converting of seats characterised by the arrangement of electric motors for adjustment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0649—Seats characterised by special features for reducing weight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0696—Means for fastening seats to floors, e.g. to floor rails
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D2011/0046—Modular or preassembled units for creating cabin interior structures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D2011/0053—Cabin passenger reading lights
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
Definitions
- the present invention relates to a module, a system and a method for aircrafts, the use of a module in an aircraft and to an aircraft.
- Today's commercial aircraft cabins are designed to accommodate passengers and their luggage by providing several distinct and largely independent components. More precisely, the individual passenger cabin environment is made up of seats, for instance including underseat stowage, life vests, information placards, literature pouches, plus overhead stowage bins including passenger service units, for instance reading lights, air outlets, information signs, loudspeakers and supplemental oxygen.
- seats for instance including underseat stowage, life vests, information placards, literature pouches, plus overhead stowage bins including passenger service units, for instance reading lights, air outlets, information signs, loudspeakers and supplemental oxygen.
- Aircraft provisions for the attachment of seats are typically provided via floor structure with limited incremental positioning.
- Overhead stowage bins are installed in a fixed location and provide accommodation for PSU (Passenger Service Unit) components.
- PSU Passenger Service Unit
- DE 43 01 681 C1 describes a satellite like a PSU which can be shifted in longitudinal direction without disrupting any of its functions. All PSU functions are fed to the PSU.
- DE 195 02 658 C1 describes essentially the same functional principles for satellites, but the unit is supported by a flexible arm that allows the PSU to give way to the opening of a pivoting bin.
- DE 195 33 981 C1 reveals an arrangement with PSU functions around the individual passenger seat and unfolds a privacy umbrella when the seat is reclined. The feeding of the PSU function allowing for layout changes.
- DE 195 34 025 discloses PSU functions around the passenger seat and is designed in a column. The column can be part of the transversal seat structure or is separate flats transversal elements on the floor either in front of the seat or behind it and companying the seat roll without functional disruption when it is moved for a change of layout.
- US 5,716,026 relates to a split-level seating device for elevating and mounting alternate rows of seats for aircraft, surface transportation or for stationary applications, as a means to gain greater seating comfort and to increase overall seating capacity, by preempting otherwise unutilized or inefficient spatial displacement within such vehicles, to enable every sitter a lower seating position and every sitter to raise the legs at or above the level of the torso.
- a modular pedestal raises every other row of seats with their corresponding cross-aisle walkways at a sufficient height to provide legroom for floor level sitter, said module incorporating a legrest extension for upper level sitter, including the means for affixing state-of-the-art safety, sanitary and conveniency devices, such as safety crash-absorbing air bags and high-security kevlar lining, oxygen dispensers, purge vents and ultra-violet light outlets to cleanse the environment, moveable and adjustable footrests, eating-writing surfaces, and audio-visual entertainment and communications devices.
- the manner following convention of mounting arrays of massed seats at floor level is improved upon by elevating alternate rows of seats by means of said modular devices, all seats, both floor and split-level, being accessed from the same floor surface.
- the object may be solved by a module according to claim 1, by a system according to claim 20 and by a method for an aircraft according to claim 21, by the use of the module in an aircraft according to claim 24 and by an aircraft comprising the module.
- a module for an aircraft wherein the aircraft having a fuselage structure and a floor element.
- the floor element is defining a floor plane.
- the Module comprises a frame device wherein the frame device is adapted for mounting a functional element. Further, the frame device is adapted for attachment to the floor element of the aircraft at a first location in the floor plane and the frame device is adapted for attachment to the fuselage structure of the aircraft at a second location. Thereby, the second location is not in the floor plane.
- a system for providing a module for an aircraft comprises a plurality of modules according to the present invention and a control unit.
- the plurality of modules is adapted to be movable electrically, wherein the control unit is adapted to control the plurality of modules in such a way, that each of the plurality of modules is movable along a fuselage.
- a method for is provided.
- a functional element is mounted to a frame device.
- the frame device is attached to a floor element of the aircraft at a first location in the floor plane and further on, the frame device is attached to the fuselage structure of the aircraft at a second location.
- the floor element is defining a floor plane, wherein the second location is not in the floor plane.
- the expression "functional element” shall define for instance all installations in the cabin of an aircraft, that are installed in the environment of the passenger, such as seats, stowage bins, monuments, galleys, lavatories, movable class dividers, PSU's (passenger service units), lighting, air condition, loudspeakers, televisions, computers and oxygen masks etc..
- the wording fuselage structure shall define for instance the fuselage skin, the aircraft frames, the aircraft stringers or the cabinrelated parts.
- the wording floor element shall define for instance the different floor levels inside an aircraft.
- the frame device surrounds the functional element.
- the frame device is connected to the functional element by at least two connection points, whereby the connection points are not located in the same plane.
- the frame device surrounds the centre of gravity of the functional element, so that the an optimized load distribution of acceleration forces can be provided and torques reduced or avoided.
- the frame device provides more stability. If a connecting line between two connecting points of the frame device to the functional element runs through the centre of gravity of the functional element an optimized load distribution of the functional element can be provided.
- the frame device is adapted for a slideable attachment to the floor element of the aircraft and the fuselage structure, such that the frame device is relocatable from a first position in the aircraft by a sliding movement to a second position in the aircraft.
- the second position is at a distance in the longitudinal direction of the aircraft from the first position.
- a very flexible cabin layout can be provided.
- many functional elements like oxygen masks, seats or air condition are often fixed to the floor elements or the fuselage structure.
- the functional elements in the overhead area have to be changed accordingly to the new seat position.
- the functional elements in the overhead area are fixed to the floor structure, so that it is very complicated to change their position.
- the functional element is attached by an attachment element to a relocatable frame device.
- This frame device can be fixed to the primary aircraft structure or the secondary structure, such as the cabin related parts and the floor in such a way, that in case of changing the cabin layout or position of all functional elements, for instance a seat position, a further functional element for instance a stowage bin, will be repositioned automatically by changing the position of the frame device.
- a new cabin layout can be configured rapidly.
- airliners could be able to adapt the capacity of their cabin layouts, such as for instance business or economy class layouts, to the amounts of the tickets sold for each class. Therefore, by changing the position of each module in a very short period of time, flexible capacities of i.e. business class or economy class can be configured by enlarging or reducing the distance between the modules respectively the seats. Very short turnaround times and an optimized utilization can be provided.
- the floor element of the aircraft and the fuselage structure comprise a rail element.
- the rail element is adapted for mounting the frame device slideable in such a manner, that the frame device is relocatable along the rail element.
- an efficient construction is provided to remove the module easily in direction of the rail.
- a plurality of rails can be provided on a plurality of connection points around the frame device in order to reinforce the fixation of the module.
- the module can easily slide so that the reconfiguration time can be shortened.
- the module further comprises a damper element.
- the damper element is thereby attached between the module and at least to one of the fuselage structure and the floor element.
- the damper element is adapted to reduce for instance the acceleration forces, that affect the module for instance in case of a 16 g crash deceleration. Therefore the maximum loads can be reduced by the damper element, so that the forces respectively acceleration/ deceleration loads at the connection points between the module and the fuselage or floor are minimized.
- the damper element is located in the rail element or in the frame device.
- the module further comprises an adapting element, whereby the adapting element is located between the module and at least to one of the fuselage structure and the floor element.
- the adapting element can for instance consist of a flexible lever or telescoping halves of a frame device.
- the functional element is movable in respect to the frame device.
- each position of the functional element can be placed individually along the frame device.
- the height or the longitudinal position can be changed individually.
- the height of the stowage bin can be configured individually so that for instance smaller persons can access the stowage bin more easily.
- constructive elements for instance by fixing the attachment element to the frame device eccentrically.
- other constructions such as rails or a snap construction can be provided.
- the frame device comprises a plurality of frame elements, wherein the frame elements are mounted detachably.
- the measures of the frame element can be designed individually.
- the installation of the modules it is much easier to carry the single frame elements into the aircraft than the whole frame device itself. Therewith the assembly and the installation of the frame device including the functional elements can be eased enormously.
- the frame elements can be connected adjustable.
- an already installed frame device including the plurality of frame elements can be adjusted easily without reassembling the frame.
- the frames of the module have to be adjusted in case of sliding the modules along a fuselage.
- the plurality of frame elements are designed telescopically for providing for instance flexible measures of the frame device.
- the frame elements can also be adapted to be foldable.
- each frame element of the plurality of frame elements has a different shape in comparison to the plurality of frame elements.
- a plurality of different shapes of the frame device can be accomplished, so that very flexible installations of the module in a fuselage of an aircraft can be provided.
- Favourite shapes in frame elements or frame device configurations can be closed, surrounding frame shapes, such as circles, rectangles or other closed shapes, but also open shaped frames like for instance frames with a C-shape, G-shape, I-shape, L-shape, A-shape, H-shape or T-shape etc..
- the module is adapted to be connectable to a primary aircraft structure in such a manner, that the module absorbs loads from the primary aircraft structure.
- Primary aircraft structure defines all fuselage parts that are supporting the structure of a fuselage, such as frames and stringers. Therewith the functions of the fuselage primary structure and the frame device according to the present invention can be combined.
- the inventive module of this embodiment can reinforce the primary aircraft structure.
- most of the structural frames or stringers can be combined or integrally performed with a module according to the present invention, so that the total weight of the structure and the costs can be reduced.
- the frame device is shaped in such a way, that the frame device conforms with the shape of at least one of the fuselage structure and the floor element.
- the frame device can be installed very space-saving in the aircraft fuselage and additionally no disturbing elements, such as frame pillars, can be recognized by the passengers.
- the functional element is mounted modularly to the frame device.
- the functional element can be replaced individually.
- a seat device as first functional element, it can be very useful to exchange business class seats with economy class seats.
- the airliners can exchange easily and very fast the toilet instead of a row of seats.
- the airplane can provide more efficiency, because every airline can adapt cabin layouts according to their own needs.
- the functional element consists of a transversal stowage bin.
- the transversal stowage bin comprising an opening for placing items in the transversal stowage bin, wherein the aircraft has a longitudinal direction in or against flight direction and wherein the opening is accessible in or against flight direction.
- loading or unloading luggage into/ out of the stowage bins is very time consuming, because the openings of the stowage bins are accessible from the aisle of the cabin, respectively from an orthogonal direction to the longitudinal direction of the fuselage respectively to the flight direction. In case that one passenger tries to put items into the stowage bins it is impossible for other passengers to bypass this passenger along the aisle.
- each passenger can have his individual transversal stowage bin, that is operable from the transversal passage way between two neighbouring seat rows. Additionally by using this inventive transversal stowage bin assembly, it is possible to provide more space between the seat rows , because no overhead elements need to be installed above the transversal passage way between two seat rows. Thus, there is also more available space for each passenger. Further on, by installing separation walls in the transversal stowage bin, an individual stowage bin for each passenger can be provided.
- the stowage bin comprises at least one functional tool, wherein the at least one functional tool is selected from the group consisting of lighting, air condition, loudspeakers, televisions, computers and oxygen masks.
- these functional tools can be fixed to the functional elements such as the stowage bin. Therewith by moving or relocating the module including the stowage bins, all functional tools will also be repositioned.
- the functional tools can also be fixed integrally or removable with a stowage bin.
- the functional element consists of a seat element.
- the seat element is adapted to be foldable, so that modules that are not in use can be pushed together and placed in a space-saving manner at one end of the cabin. For instance, if more first or business class seats are required, also more space between the modules respectively the seat rows is required, so that the excessive modules have to be stored in the cabin end. By folding the seats or also the stowage bins more modules can be stored easily.
- At least one of the first functional element and the second functional element is selected from the group of monuments, galleys, lavatories, PSUs, lighting, air condition, loudspeakers, televisions, computers and oxygen masks.
- the module further comprises a supply connection for supplying at least one of the first functional element and the second functional element wherein the supply connection is adapted to be engageable with supply elements of the fuselage.
- a rail can be provided on the fuselage side to keep sliding contact in case the module is repositioned.
- the frame device comprises a plurality of functional elements, for instance by using seats as a first functional element and stowage bins as second functional element, a frame device according to this exemplary embodiment can provide for instance a row of a random number of seats and a random number of stowage bins. By relocating the module, also all seats and stowage bins will be relocated in the same step. Also the desired amounts of other kinds of functional elements can be attached to one frame device.
- the module comprises a plurality of frame devices.
- a module having an upper frame device including a functional element, for instance, a stowage bin and lighting, and having a second frame device including seats.
- a functional element for instance, a stowage bin and lighting
- a second frame device including seats.
- Usable materials for frame devices can consist of carbon fibre, aluminium or various composite fibres, glare etc..
- an adapting element adapts to the relative movements between the module and the fuselage.
- a plurality of frame elements of the frame device is connected adjustably for providing flexible measures of the frame device.
- the plurality of frame elements is modularly connected, wherein each frame element of the plurality of frame elements has a different shape in consideration to the plurality of frame elements.
- the module is connected to the primary aircraft structure for absorbing loads in such a manner, that the module is part of the primary aircraft structure.
- the functional element is mounted modularly for being exchangeable.
- the functional element is supplied in such a way, that a supply connection of the module is connected with supply elements of at least one of the fuselage structure and the floor element.
- a feeder rail principle By using a feeder rail principle, a sliding contact between the module and the fuselage can be provided.
- the frame device can be operated electrically for moving the module along at least one of the fuselage structure and the floor elements by means of a control unit.
- the module having the above-mentioned features is used in an aircraft.
- an aircraft comprising a module having the above mentioned features is provided.
- the exemplary embodiments of the module are also valid for the system and the method as well as for the use and the aircraft and inversely.
- FIG. 1 to 3 illustrate schematic views of exemplary embodiments of the present invention.
- a module for an aircraft is shown, wherein the aircraft having a fuselage structure 6 and a floor element 5.
- the floor element 5 defining a floor plane.
- the module comprises a frame device 2 wherein the frame device 2 is adapted for mounting a functional element 4.
- the frame device 2 is adapted for attachment to the floor element 5 of the aircraft at a first location 7 in the floor plane and wherein the frame device 2 is adapted for attachment to the fuselage structure 6 of the aircraft at a second location 7'.
- the second location 7' is thereby not in the floor plane.
- a rail element 8 whereby the frame device 2 can be fixed relocatable respectively movable to the rail 8.
- an aircraft seat 14 or an overhead stowage bin 11 as functional element 4
- an easy relocation of the whole module 1 can be provided.
- all necessary overhead functional elements such as oxygen masks, lighting or air condition need to be adapted separately to the new seat position.
- the overhead functional elements 4, 11 will be relocated automatically.
- Fig.1 shows thereby an open frame shape 2, wherein Fig 2 and 3 illustrate a closed frame shape 2.
- Fig 2 and 3 illustrate a closed frame shape 2.
- Fig. 3 shows a exemplary embodiment of supported standing places for passengers.
- the centre of gravity of the passengers body is thereby very high above the floor 5, so that by fixing the support 14 just on the floor section 3 will lead to high torques.
- the frame device 2 By means of the frame device 2 the frame surround the centre of gravity, so that high torques are avoided.
- Fig. 4 illustrates a damper element 3 integrated in a rail in order to absorb 16g loads.
- Fig. 5 shows a schematic view of a damper integrated in a frame device in order to absorb 16 g loads
- Fig. 6 shows a schematic total view of a frame device 2 of a module 1, which is movably connected to the rail element 8.
- a plurality of connection elements 3 that are connected to the rail elements 8 can be provided in order to reinforce the connection between the module 1 and the fuselage 6.
- Fig. 6 illustrates an open frame 2 with its open portion at the upper end of the surrounded area and hence describing a U-shape that allows the use of the module 1 in combination with a conventional longitudinal bin 11.
- the typical layout flexibility of the module is provided by all functional elements of a PSU being contained in a horizontal beam that is connected to the U-shaped frame 2.
- Fig. 7 shows an exemplary construction for attaching the module 1 relocatably and moveable to the fuselage structure 6 and the floor element 5.
- Rails it is possible to provide an easy constructive method for moving the frame devices 2 respectively the module 1.
- Connection elements 3 may be fixed to the frame device and are movably engaged with the rail 8.
- the frame device 2 provides thereby a closed, surrounding shape.
- Fig. 8 and 9 illustrate a frame device 2 that is connected to a fuselage 6, wherein an additional adapting element 9 is included.
- the adapting element 9 is connected to the frame device for adapting relative movements between the fuselage 6 and the frame device 2.
- Fig. 8 the frame device 2 adapts to the relative movements of the fuselage structure 2 by means of an adapting lever 9.
- Fig.9 shows a schematic view of an exemplary adapting system of the module to the relative movement of the fuselage by means of a telescoping element within the frame device.
- Fig. 10 and 11 show a further exemplary embodiment of the present invention whereby the functional elements 4, 5 can be relocatably fixed to the frame device 2.
- the functional element 4 is fixed thereby adjustable to the frame device 2 to enable an adjustment.
- simple constructions can be provided, for instance by connecting the attachment elements or the functional elements eccentrically to the frame device 2.
- the functional elements here for instance the seats or the stowage bins, can be adjustable in height.
- Fig. 11 shows a more detailed view of an adjustable seat 14 that is adjustably mounted to the frame device 2.
- Fig. 12 shows an exemplary view of a seat layout with reduced seat pitch made possible thanks to an increased seat height.
- the increased seat height allows for an increased luggage volume below the seats.
- Fig. 12' shows an exemplary view of a seat layout with increased seat pitch but reduced seat height for more comfort.
- the modules not in use are stowed away in one end of the cabin.
- Figs. 13 to 15 are showing some exemplary embodiments of different frame shapes.
- Fig. 13 illustrates a closed, surrounding frame device 2 consisting of several frame elements 10.
- the frame elements 10 form two closed frames, wherein in the upper rectangle frame a stowage bin 11 can be located and in the lower rectangle a seat row 14 can be installed as shown in Fig. 13' .
- Figs. 14 and 14' show an open frame device consisting of frame elements 10 with an open shape, here in a C-shape.
- a step is provided wherein in the lower stage provides a functional element 4, for instance a seat element 14, and in the upper stage a stowage bin 11 for storing items.
- Figs. 15 and 15' show a further shape of the frame device 2 consisting of several frame elements 10 wherein a lower section builds a C-shape but also containing an upper section.
- a functional element 4 can be placed, for instance a seat element 14, whereas in the upper section a stowage bin 11 can be placed as a functional element 4.
- Fig. 16 and show a front view of a cross-section of a fuselage, wherein Fig 16 . shows a three level fuselage layout.
- all differently shaped frame devices 2 are installed for the various purposes.
- the shape of the frame device shown in Fig. 10 is installed on the right and the left side for providing an optimal cabin layout with optimized space saving installation.
- the middle of the second and third level frame devices according to Fig. 8 , 8' are installed for providing a space-saving cabin layout.
- Fig. 17 shows a single deck two aisle fuselage cross-section equipped with open frame modules 1. The open portion of the respective frame is adjacent to the respective aisle.
- Fig. 18 and 19 show three-dimensional views of cabin layouts according to an exemplary embodiment of the present invention.
- the frame devices 2 are curved either in longitudinal direction of the fuselage 6 or in such a way to conform to the shape of the sidewalls of the fuselage 6.
- the frame devices 2 By curving the frame devices 2 in a longitudinal direction of the fuselage 6, the field of vision of the passengers will be optimized.
- the frame shape of the frame device 2 with the fuselage structure 6 the available space in the cabin will be optimized and disturbing frame parts can follow the contour of the side panels of the aircraft structure.
- the frame shape can either be opened to the aisle side or the window side.
- the aisle between the seat rows can be kept free of any overhead elements such as stowage bins or oxygen masks, so that the available height increases the comfort level for the passengers.
- Figs. 20 and 20' show an exemplary embodiment of the present invention wherein the stowage bins 11 are accessible in longitudinal direction of the fuselage.
- the aisle between the seats 14 in longitudinal direction can be kept free..
- the turnaround time can be shortened.
- individual stowage bins 11 for each passenger can be provided.
- the overhead stowage compartments 11 can be designed as fixed bins with a floor and an upper hinged lid to give access when stowing luggage or as movable bins which move downward around a pivot or by various kinematics like parallelograms or others. Luggage can also be stored under the passenger seats.
- Fig. 21 shows an exemplary embodiment of a supply system for the functional elements 4 or the functional tools 13.
- a supply connection 15 is fixed to the frame device 2, that can be adapted to be engageable with a supply element 16 of the fuselage structure 6.
- the supply connection 15 will remain connected with the supply element 16 of the fuselage.
- the supply connection 16 can be designed like a rail, including for instance air or electricity lines.
- the supply connection 15 of the module can be in slideable contact with the feeder-rail 16 and respectively in slideable contact with the supply sources.
- Fig. 22 shows a fuselage 6' wherein the frame devices 2 of the modules 1' are installed rigidly with the fuselage primary structure 6'.
- the fuselage frames can be built integrally with the frame device 2', so that weight and complexity of the fuselage construction can be reduced.
- Figs. 23 and 24 are showing further exemplary embodiments of the module 1 comprising a plurality of frame devices 2.
- an upper frame device 2 is shown, wherein a functional element 4; 11 is installed.
- An independent second frame device 2' is installed on the lower side of the module 1 wherein a second functional element 4; 14 is installed.
- the upper and lower frame devices 2, 2' can be relocated independently.
- Fig. 23 illustrates a foldable seat element 14' for reducing the space requirements for a module 1.
- Fig. 24 shows an exemplary embodiment of an installation of a stowage bin 11.
- the frame device 2 is connected to a rail element 8 by connection elements 3.
- the connection elements 3 are fixed to the fuselage structure 6 by two connecting points 3.
- the connecting line between the connecting points 3 runs through the centre of gravity of the stowage bin 11 in order to optimize the load distribution of the stowage bin 4, 11 and to minimize the torques.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Body Structure For Vehicles (AREA)
- Seats For Vehicles (AREA)
- Vibration Prevention Devices (AREA)
- Details Of Aerials (AREA)
Claims (25)
- Module pour un aéronef, l'aéronef comportant une structure de fuselage (6) et un élément plancher (5) ; l'élément plancher (5) définissant un plan de sol, le module comprenant :un dispositif cadre (2) ;une pluralité d'éléments fonctionnels (4) ;dans lequel un premier élément fonctionnel est un siège (14) et un second élément fonctionnel est un porte-bagages (11) ;dans lequel le dispositif cadre (2) est conçu pour le montage des éléments fonctionnels (4) ;dans lequel le dispositif cadre (2) est conçu pour être fixé à l'élément plancher (5) de l'aéronef à un premier emplacement (7) dans le plan de sol ;dans lequel le dispositif cadre (2) est conçu pour être fixé à la structure de fuselage (6) de l'aéronef à un second emplacement (7') ; dans lequel le second emplacement (7') n'est pas le plan de sol ; etdans lequel le dispositif cadre (2) est conçu pour être fixé de façon coulissante sur l'élément plancher (5) de l'aéronef et sur la structure de fuselage (6), de sorte que le dispositif cadre (2) puisse être déplacé d'une première position dans l'aéronef, par un mouvement coulissant, à une seconde position dans l'aéronef, dans lequel la première position est à une certaine distance dans la direction longitudinale de l'aéronef de la seconde position, caractérisé en ce que le dispositif cadre est un cadre de forme fermée et entoure lesdits éléments fonctionnels (4).
- Module selon la revendication 1, dans lequel l'élément plancher (5) de l'aéronef et la structure de fuselage (6) comprennent un élément formant un rail (8) ;
dans lequel l'élément rail (8) est conçu pour le montage coulissant du dispositif cadre (2). - Module selon la revendication 1 ou 2, comprenant en outre :un élément amortisseur (9) ;dans lequel l'élément amortisseur (9) est fixé entre le dispositif cadre (2) et au moins l'un de la structure de fuselage (6) et de l'élément plancher (5).
- Module selon la revendication 2 ou 3, dans lequel l'élément rail (8) comprend un élément amortisseur (3) destiné à réduire les charges.
- Module selon l'une quelconque des revendications 1 à 4, dans lequel le module comprend en outre un élément d'adaptation (9),
dans lequel l'élément d'adaptation (9) est situé entre le dispositif cadre (2) et au moins l'un de la structure de fuselage (6) et de l'élément plancher (5) de façon à adapter les mouvements relatifs entre le dispositif cadre (2) et la structure de fuselage (6). - Module selon l'une quelconque des revendications 1 à 5, dans lequel l'élément fonctionnel (4) est mobile par rapport au dispositif cadre (2).
- Module selon l'une quelconque des revendications 1 à 6, dans lequel le dispositif cadre (2) comprend une pluralité d'éléments de cadre (10) ;
dans lequel les éléments de cadre (10) sont montés amovibles. - Module selon la revendication 7, dans lequel la pluralité d'éléments de cadre (10) sont reliés de façon réglable.
- Module selon la revendication 7, dans lequel la pluralité d'éléments de cadre (10) sont conçus pour être télescopiques et réglables.
- Module selon l'une quelconque des revendications 4 à 9, dans lequel l'élément amortisseur (9) est fixé entre les éléments de cadre (10).
- Module selon l'une quelconque des revendications 1 à 10, dans lequel le module (1) est conçu pour pouvoir être relié à une structure principale d'aéronef (6') de telle manière que le module (1) absorbe les charges de la structure principale d'aéronef (6').
- Module selon l'une quelconque des revendications 1 à 11, dans lequel le dispositif cadre (2) est formé de façon à se conformer à une forme d'au moins l'un de la structure de fuselage (6) et de l'élément plancher (5).
- Module selon l'une quelconque des revendications 1 à 12, dans lequel le dispositif cadre (2) est conçu pour le montage modulaire de l'élément fonctionnel (4).
- Module selon l'une quelconque des revendications 1 à 13, dans lequel le porte-bagages transversal comprend une ouverture (12) destinée à placer des articles dans le porte-bagages transversal (11) ;
dans lequel l'ouverture (12) est accessible dans ou contre une direction de vol. - Module selon l'une quelconque des revendications 1 à 14, le porte-bagages transversal (11) comprenant :au moins un outil fonctionnel (13),dans lequel l'au moins un outil fonctionnel (13) est sélectionné parmi un groupe constitué par l'éclairage, la climatisation, les haut-parleurs, la télévision, les ordinateurs et les masques à oxygène.
- Module selon l'une quelconque des revendications 1 à 15, dans lequel l'élément siège (14) est conçu pour être pliable.
- Module selon l'une quelconque des revendications 1 à 13, dans lequel l'élément fonctionnel (4) est sélectionné parmi le groupe constitué par les monuments, l'office, les toilettes, les blocs service passagers, l'éclairage, la climatisation, les haut-parleurs, la télévision, les ordinateurs et les masques à oxygène.
- Module selon l'une quelconque des revendications 1 à 17, le module comprenant en outre :une connexion d'alimentation (15) pour alimenter l'élément fonctionnel (4) ;dans lequel la connexion d'alimentation (15) est conçue pour pouvoir venir en prise avec des éléments d'alimentation (16) d'au moins l'un de la structure de fuselage (6) et de l'élément plancher (5), etdans lequel la connexion d'alimentation (15) est en contact coulissant avec les éléments d'alimentation (16) pour l'alimentation de l'élément fonctionnel (4).
- Module selon l'une quelconque des revendications 1 à 18, dans lequel le module (1) comprend en outre une pluralité de dispositifs cadres (2).
- Système de fourniture de modules pour un aéronef, le système comprenant :une pluralité de modules (1, 1') selon l'une quelconque des revendications 1 à 19 ; etune unité de commande ;dans lequel la pluralité de modules (1, 1') sont conçus pour pouvoir se déplacer électriquement ;dans lequel l'unité de commande est conçue pour commander la pluralité de modules (1, 1').
- Procédé pour un aéronef, le procédé comprenant :le montage d'une pluralité d'éléments fonctionnels (4) sur un dispositif cadre (2) ;dans lequel un premier élément fonctionnel est un siège (14) et un second élément fonctionnel est un porte-bagages (11) ;dans lequel le dispositif cadre est un cadre de forme fermée et entoure lesdits éléments fonctionnels (4) ;la fixation du dispositif cadre (2) sur un élément plancher (5) de l'aéronef en un premier emplacement (7) dans le plan de sol ;la fixation du dispositif cadre (2) à la structure de fuselage (6) de l'aéronef en un second emplacement (7') ; dans lequel l'élément plancher (5) définit un plan de sol ; dans lequel le second emplacement (7') n'est pas le plan de sol ; etdans lequel le dispositif cadre (2) est conçu pour une fixation coulissante sur l'élément plancher (5) de l'aéronef et sur la structure de fuselage (6), de sorte que le dispositif cadre (2) puisse être déplacé d'une première position dans l'aéronef, par un mouvement coulissant, à une seconde position dans l'aéronef, dans lequel la première position est à une certaine distance dans la direction longitudinale de l'aéronef de la seconde position.
- Procédé selon la revendication 21, comprenant en outre :
l'adaptation de mouvements relatifs au moyen d'un élément d'adaptation (9) entre le module (1) et au moins l'un de la structure de fuselage (6) et de l'élément plancher (5). - Procédé selon la revendication 21 ou 22, comprenant en outre :
la liaison réglable d'une pluralité d'éléments de cadre (10) au dispositif cadre (2). - Utilisation d'un module (1) selon l'une quelconque des revendications 1 à 19 dans un aéronef.
- Aéronef comprenant un module (1) selon l'une quelconque des revendications 1 à 19.
Priority Applications (13)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP05028664.0A EP1803645B1 (fr) | 2005-12-29 | 2005-12-29 | Module pour un aéronef |
EP06841173.5A EP1966046B1 (fr) | 2005-12-29 | 2006-12-27 | Module pour un aéronef |
EP13180763.8A EP2664541A3 (fr) | 2005-12-29 | 2006-12-27 | Module pour un aéronef |
PCT/EP2006/012545 WO2007073938A1 (fr) | 2005-12-29 | 2006-12-27 | Module pour aeronef |
JP2008547897A JP2009522148A (ja) | 2005-12-29 | 2006-12-27 | 航空機用モジュール |
BRPI0620799-5A BRPI0620799A2 (pt) | 2005-12-29 | 2006-12-27 | módulo para uma aeronave |
CN2006800499494A CN101351384B (zh) | 2005-12-29 | 2006-12-27 | 用于飞行器的模块 |
US12/087,328 US9010686B2 (en) | 2005-12-29 | 2006-12-27 | Module for an aircraft |
RU2008130999A RU2414389C2 (ru) | 2005-12-29 | 2006-12-27 | Модуль для воздушного судна и способ его формирования |
CA 2632276 CA2632276A1 (fr) | 2005-12-29 | 2006-12-27 | Module pour aeronef |
US11/618,303 US20070152480A1 (en) | 2005-12-29 | 2006-12-29 | Luggage Retention Device and Seat with Such a Luggage Retention Device |
US11/618,290 US7922119B2 (en) | 2005-12-29 | 2006-12-29 | Telescopic stowage bin |
US14/660,268 US20150259067A1 (en) | 2005-12-29 | 2015-03-17 | Module for an aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP05028664.0A EP1803645B1 (fr) | 2005-12-29 | 2005-12-29 | Module pour un aéronef |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1803645A1 EP1803645A1 (fr) | 2007-07-04 |
EP1803645B1 true EP1803645B1 (fr) | 2020-03-11 |
Family
ID=36581853
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP05028664.0A Not-in-force EP1803645B1 (fr) | 2005-12-29 | 2005-12-29 | Module pour un aéronef |
EP13180763.8A Withdrawn EP2664541A3 (fr) | 2005-12-29 | 2006-12-27 | Module pour un aéronef |
EP06841173.5A Not-in-force EP1966046B1 (fr) | 2005-12-29 | 2006-12-27 | Module pour un aéronef |
Family Applications After (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13180763.8A Withdrawn EP2664541A3 (fr) | 2005-12-29 | 2006-12-27 | Module pour un aéronef |
EP06841173.5A Not-in-force EP1966046B1 (fr) | 2005-12-29 | 2006-12-27 | Module pour un aéronef |
Country Status (8)
Country | Link |
---|---|
US (2) | US9010686B2 (fr) |
EP (3) | EP1803645B1 (fr) |
JP (1) | JP2009522148A (fr) |
CN (1) | CN101351384B (fr) |
BR (1) | BRPI0620799A2 (fr) |
CA (1) | CA2632276A1 (fr) |
RU (1) | RU2414389C2 (fr) |
WO (1) | WO2007073938A1 (fr) |
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2005
- 2005-12-29 EP EP05028664.0A patent/EP1803645B1/fr not_active Not-in-force
-
2006
- 2006-12-27 BR BRPI0620799-5A patent/BRPI0620799A2/pt not_active IP Right Cessation
- 2006-12-27 US US12/087,328 patent/US9010686B2/en active Active
- 2006-12-27 EP EP13180763.8A patent/EP2664541A3/fr not_active Withdrawn
- 2006-12-27 EP EP06841173.5A patent/EP1966046B1/fr not_active Not-in-force
- 2006-12-27 JP JP2008547897A patent/JP2009522148A/ja active Pending
- 2006-12-27 WO PCT/EP2006/012545 patent/WO2007073938A1/fr active Application Filing
- 2006-12-27 CA CA 2632276 patent/CA2632276A1/fr not_active Abandoned
- 2006-12-27 RU RU2008130999A patent/RU2414389C2/ru not_active IP Right Cessation
- 2006-12-27 CN CN2006800499494A patent/CN101351384B/zh not_active Expired - Fee Related
-
2015
- 2015-03-17 US US14/660,268 patent/US20150259067A1/en not_active Abandoned
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Also Published As
Publication number | Publication date |
---|---|
CN101351384B (zh) | 2010-09-29 |
EP1966046A1 (fr) | 2008-09-10 |
WO2007073938B1 (fr) | 2007-08-09 |
EP1803645A1 (fr) | 2007-07-04 |
EP1966046B1 (fr) | 2019-04-17 |
EP2664541A2 (fr) | 2013-11-20 |
RU2414389C2 (ru) | 2011-03-20 |
US20090283636A1 (en) | 2009-11-19 |
JP2009522148A (ja) | 2009-06-11 |
EP2664541A3 (fr) | 2017-12-13 |
US9010686B2 (en) | 2015-04-21 |
US20150259067A1 (en) | 2015-09-17 |
RU2008130999A (ru) | 2010-02-10 |
CN101351384A (zh) | 2009-01-21 |
CA2632276A1 (fr) | 2007-07-05 |
BRPI0620799A2 (pt) | 2011-11-22 |
WO2007073938A1 (fr) | 2007-07-05 |
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